Eurocopter EC 635
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| EC 635 | |
|---|---|
| Type | Light Multi-Purpose Helicopter |
| Manufacturer | Eurocopter |
| Introduced | May 1998 |
| Primary users | Royal Jordanian Air Force Swiss Air Force |
| Number built | 31 |
| Developed from | Eurocopter EC 135 |
The Eurocopter EC 635 is a light multi-purpose helicopter developed by Eurocopter as a military version of the Eurocopter EC 135. It is a twin-engined aircraft and can carry up to 8 people, including the pilot, and a range of military equipment or armaments. The helicopter is marketed for troop transport, medical evacuation, cargo transport and armed combat support missions.
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[edit] Development
The Eurocopter EC 635 was developed to meet a Portuguese Army requirement for a fire support and medical evacuation helicopter to support its plans for a specialist Army Air Corps unit — UALE. The EC 635 was first revealed at the Aviation Africa exhibition in May 1998 and the Portuguese Ministry of Defence subsequently signed an agreement for nine EC 635 T2 helicopters equipped with Turbomeca Arrius 2B2 engines, at a cost of €35 million in October 1999.[1] Delivery of the first Portuguese aircraft was expected to begin in 2001, however, continual delays in production led to the Portuguese Ministry of Defence canceling the contract in August 2002, citing Eurocopters failure to deliver all aircraft between August 2001 and April 2002 as the reason. Eurocopter claimed that disagreements over the integration of weapons systems on the helicopter were the reason for the cancellation.[2]
The Royal Jordanian Air Force agreed to purchase the 9 Portuguese helicopters in October 2002 and the first aircraft was delivered in July 2003. Jordan ordered a further 4 helicopters in January 2006 and deliveries of all machines were completed in 2007.
In April 2006, the Swiss Defence Procurement Agency (Armasuisse) ordered 18 EC 635's for the Swiss Air Force, to replace the aging Aérospatiale Alouette III in performing transport and advanced training missions. The first two aircraft will be built by Eurocopter, with the remaining 16 being built by RUAG Aerospace in Alpnach, Switzerland and deliveries expected to be completed between March 2008 and December 2009.[3]
[edit] Design
The EC 635 is based on the Eurocopter EC 135, improving upon the design for military operations and able to carry weapons systems. The helicopter is fitted with a choice of powerplants, depending on customer requirements and can be powered by two Pratt & Whitney PW206B2 turbine engines or two Turbomeca Arrius 2B2 turbine engines. The powerplant is mounted over the cabin and features a Full Authority Digital Engine Control system. The engines power a fibre-reinforced composite Bearingless Main Rotor (BMR) with four blades, and the familiar Fenestron enclosed tail rotor, both of which reduce vibration and noise levels. Vibration levels are further reduced by a built-in Anti Resonance Isolation System (ARIS). The EC 635 can be fitted with either a conventional cockpit consisting of a traditional dashboard, or a glass cockpit, which utilizes a Thales "Avionique Nouvelle" suite with MEGHAS Flight Control Display System and active matrix liquid crystal displays.
There are four configurations designed by Eurocopter for the EC 635. The Troop Transport version can be fitted with utility seats to carry up to 7 troops with a pilot, or passenger seats to carry up to 6 people and a pilot. The Medical Evacuation version can carry 1 or 2 litters with up to 5 seated medical workers. The Cargo Transport version has 4.9 m³ (173.04 ft³) of space for cargo, while the Armed Mission version is equipped with specialist equipment and weapons for combat. The helicopter can also be fitted with a FLIR camera turret, an infra-red capable search light, SAR weather radar and electronic equipment for Observation Missions.
The EC 635 can carry two side-mounted Multi-Purpose Pylons with aerodynamic fairings for weapons systems and can be fitted with the following military equipment and weapons:
- 2 x 70mm (2.75") FN-Herstal FZ321 12-tube rocket launchers mounted on each side.
- 2 x 20mm GIAT NC621 Cannon Pods with 180 rounds each.
- 2 x 12.7mm FN-Herstal HMP-400 Machine Gun Pods with 400 rounds each.
- 7.62mm Door Gunner Post
- EADS MILDS AN/AAR-60 MIssile Launch Detection System
- Electro Chaff-Flare Dispenser System
[edit] Operational History
[edit] Variants
- EC 635 P2
- Powered by two Pratt & Whitney PW206B2 turbine engines.
- EC 635 T2
- Powered by two Turbomeca Arrius 2B2 turbine engines.
- EC 635 P2i
- With increased maximum take-off weight, useful load, maximum continuous power, take-off power and improved high-altitude plus hot temperature performance.
- EC 635 T2i
- With increased maximum take-off weight, useful load, maximum continuous power, take-off power and improved high-altitude plus hot temperature performance.
[edit] Operators
- The Royal Jordanian Air Force operates 13 EC 635 T2's for border surveillance, anti-terrorism operations, police and EMS missions.[4]
- 18 ordered by the Swiss Air Force for transport and training missions, expected to be delivered between March 2008 & December 2009.[5]
[edit] Specifications (EC 635 P2)
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.General characteristics
- Crew: 1 or 2 pilots
- Capacity: up to 7 passengers
- Length: 10.21 m (33.5 ft)
- Rotor diameter: 10.20 m (33.5 ft)
- Height: 3.62 m (11.9 ft)
- Disc area: 81.7 m² (880 ft²)
- Empty weight: 1,467 kg (3,234 lb)
- Useful load: 1,443 kg (3,181 lb)
- Max takeoff weight: 2,910 kg (6,415 lb)
- Powerplant: 2× Pratt & Whitney PW206B2 turboshafts, 609 kW (816 hp) each
Performance
- Never exceed speed: 278 km/h (150 kts)
- Maximum speed: 278 km/h (150 kts)
- Cruise speed: 261 km/h (141 kts)
- Range: 650 km (351 nm)
- Service ceiling 6,095 m (20,000 ft)
- Rate of climb: 10.9 m/s (2,150 ft/min)
[edit] Specifications (EC 635 T2)
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.General characteristics
- Crew: 1 or 2 pilots
- Capacity: up to 7 passengers
- Length: 10.21 m (33.5 ft)
- Rotor diameter: 10.20 m (33.5 ft)
- Height: 3.62 m (11.9 ft)
- Disc area: 81.7 m² (880 ft²)
- Empty weight: 1,467 kg (3,234 lb)
- Useful load: 1,443 kg (3,181 lb)
- Max takeoff weight: 2,910 kg (6,415 lb)
- Powerplant: 2× Turbomeca Arrius 2B2 turboshafts, 609 kW (816 hp) each
Performance
- Never exceed speed: 278 km/h (150 kts)
- Maximum speed: 278 km/h (150 kts)
- Cruise speed: 261 km/h (141 kts)
- Range: 635 km (343 nm)
- Service ceiling 6,095 m (20,000 ft)
- Rate of climb: 10.9 m/s (2,150 ft/min)
Armament The EC 635 can carry two side-mounted Multi-Purpose Pylons with aerodynamic fairings for weapons systems and can be fitted with the following military equipment and weapons:
2 x 70mm (2.75") FN-Herstal FZ321 12-tube rocket launchers mounted on each side.
2 x 20mm GIAT NC621 Cannon Pods with 180 rounds each.
2 x 12.7mm FN-Herstal HMP-400 Machine Gun Pods with 400 rounds each.
7.62mm Door Gunner Post
EADS MILDS AN/AAR-60 MIssile Launch Detection System
Electro Chaff-Flare Dispenser System
[edit] References
- ^ Helis.com - Nine EC 635 Helicopters For The Portuguese Army
- ^ Helis.com - Portugal Cancels EC 635 Contract
- ^ Flug Revue - Switzerland Orders 20 EC 635s
- ^ EADS N.V. - Royal Jordanian Air Force Places Order For An Additional Four EC635s
- ^ Eurocopter Press Release - First Eurocopter EC635 For Swiss Air Force Takes To The Air
[edit] External links
- Eurocopter EC 635 Technical Data Manual
- Air Force Technology - Eurocopter EC 635
- Deagel.com - EC635
- Federation of American Scientists - EC 635 Light Utility Helicopter (LUH)
- Global Security.org - EC 635 Light Utility Helicopter (LUH)
[edit] See also
Related development
Comparable aircraft
Related lists
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